Airbus A321XLR vs. Short C-23 Sherpa

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Airbus A321XLR versus Short C-23 Sherpa
44.51 m 146 ft 0 in length 17.68 m 58 ft 0 in
11.76 m 38 ft 7 in height 6.55 m 21 ft 6 in
35.8 m 117 ft 5 in wingspan 22.76 m 74 ft 8 in
CFM LEAP-1A and P&W PW1100G engines 2 x Pratt & Whitney Canada PT6A-45R turboprop engines
33,000 lbs (147 kN) thrust per engine Approximately 1,200 hp per engine
66,000 lbs (294 kN) total thrust Approximately 2,400 hp total
101,000 kg 222,700 lb MTOW 7,484 kg 16,500 lb
4,700 nmi 8,704 km range 1,048 km 566 nm
963km/h 598mph cruise speed 425 km/h 264 mph
180-220 seats (typical 2-class seating) capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.